COMPUTATIONAL METHOD FOR UNSTEADY MOTION OF TWO-DIMENSIONAL AIRFOIL
A numerical method is developed for calculation of the wake geometry and aerodynamic forces on two-dimensional airfoil under going an arbitrary unsteady motion in an inviscid incompressible flow (panel method). The method is applied to sudden change in airfoil incidence angle and airfoil oscillatio...
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| Format: | Article |
| Language: | English |
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University of Baghdad
2024-02-01
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| Series: | Journal of Engineering |
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| Online Access: | https://joe.uobaghdad.edu.iq/index.php/main/article/view/2445 |